The joint philosophies of “safe life,” “fail-safe,” and “failure safety,” are considered in the design of new rotary wing aircraft with particular regard to airline type operation. The methods of developing these characteristic in the aircraft are discussed -- including state-of-the-art and advanced concepts. The subjects include structural considerations of rotors, power transmission, airframe and landing gear; stability and control considerations; instruments and avionics; controls; and electrical and hydraulic systems. Lockheed believes these characteristics can be designed into rotary wing aircraft and thus provide flight safety that exceeds the excellent records of such operators as Los Angeles Airways, New York Airways, and San Francisco and Oakland Helicopter airlines.


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    Titel :

    Failure Safety in V/STOL Operations


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Hayes, James (Autor:in) / Nelson, Norman E. (Autor:in) / Kesling, Paul H. (Autor:in)

    Kongress:

    National Aeronautic Meeting and 3rd International Simulation and Training Conference ; 1967



    Erscheinungsdatum :

    01.02.1967




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Failure safety in V/STOL operations

    Hayes, J. / Kesling, P.H. / Nelson, N.E. | Engineering Index Backfile | 1967



    STOL in Low Density Operations

    Ausrotas, Raymond A. | SAE Technical Papers | 1973


    STOL operations in city center

    Bakke, O. | Engineering Index Backfile | 1966


    Representative Operations of V/STOL Aircraft

    Franklin, James A. | AIAA | 2002